EXPERIMENTAL ROCKET MOTOR PERFORMANCE AND HEAT TRANSFER OF THE WFNA- AMMONIA AND THE RFNA-AMMONIA PROPELLANT SYSTEMS AT COMBUSTION PRESSURES OF 1000 PSIA AND 1500 PSIA

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1957
Accession Number
AD0139275

Entities

People

  • D. G. Elliott
  • R. K. Rose

Organizations

  • Purdue University

Tags

DTIC Thesaurus Topics

  • Coefficients
  • Combustion
  • Combustion Chambers
  • Cooling
  • Diameters
  • Experimental Data
  • Flow
  • Flow Rate
  • Gas Turbines
  • Heat Transfer
  • Injectors
  • Instrumentation
  • Jet Engines
  • Liquid Rocket Oxidizers
  • Rocket Engines
  • Rocket Oxidizers
  • Test Equipment